I haven't flown a T34 but have heard they are fun!
Previously you made a comment on about rev response in a fighter wasn't as critical. The thing I'm leery of is how much throttle jockeying actually went on.
Those guys didn't have the energy to burn that you superjocks have. Once the surly bonds of earth were loosed, dancing the sky on laughter silvered wings bled off energy faster than it could be replenished. Adrenalated and imbued with "speed is life", a low time combat pilot would likely find it counter intuitive to deliberately sacrifice some in the middle of a furball. A lesson that the overweight, underpowered T34 taught me. It's a blast to fly, but hemorrhages energy like a slashed carotid in aerobatics. There's an STC to bolt a 285 HP IO520 on in place of the stock 225 HP O470, and that's what the airshow performer T34s have. Those extra 60 ponies are something to salivate over.
If the pilot is bounced while in economical cruise all bets are off. however getting that 400lb prop to rev up from 1000rpm to 1500rpm (assuming a 2:1 reduction gear) is a bigger problem than the rotating/reciprocating masses inside the engine.
SR6, thanks for the lucid clarification of prop/engine behavior in dynamic energy situations. In discussing this I tend to assume some things are self evident, and fail to explain in sufficient detail.
In the case of the surprise bounce, the adrenalated young pilot's first response is likely to be "balls to the walls", bending throttle, prop, and mixture levers over their forward stops, while the engineers back at Alison and Pratt and Wright cringe at their drafting tables.
So what happens? The engine gets a huge slug of rich mixture (which the pressure carb meters to an acceptable rate), and the prop governor's flyweights are seeking a higher RPM. This drives the prop blades to lower pitch, reducing aerodynamic rotational resistance and dedicating nearly all of the rapidly increasing engine torque to accelerating the rotating mass toward the new RPM setpoint. As the setpoint is approached, the pressure generated by the flyweights is taken up more and more by the control actuating spring and less and less by the propeller hydraulic control valve, causing the blades to drift toward a coarser pitch and aerodynamic rotational resistance to absorb more and more of the engine's torque. IF the damping of the governor is correct, rotational resistance and engine torque will come gracefully into balance at rated engine RPM. That and $10.79 will buy you an 8 oz coffee at any Starbucks in the nation. In practice, what you're likely to get in the mad scramble of a bounce turned furball is RPM overshoots and undershoots until the prop and governor catch up with themselves, and a mandatory report to your crew chief if you had the presence of mind to observe the overspeed excursion. (But don't get your posterior perforated while staring at the tach!)
Cheers,
Wes